• Search Research Projects
  • Search Researchers
  • How to Use
  1. Back to project page

2002 Fiscal Year Final Research Report Summary

Stucy on interaction between electromagnetic wave and rocket exhaust plume

Research Project

Project/Area Number 11450379
Research Category

Grant-in-Aid for Scientific Research (B)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionThe Institute of Space and Astronautical Science

Principal Investigator

OGAWA Hiroyuki  ISAS, Space Systems, Associate Professor, システム研究系, 助教授 (60311172)

Co-Investigator(Kenkyū-buntansha) KOBAYASI Yasunori  ISAS, CAST, Professor, 次世代探査機研究センター, 教授 (10132995)
HIRAKI Koju  ISAS, Space Systems, Research Associate, システム研究系, 助手 (40249933)
Project Period (FY) 1999 – 2002
KeywordsRocket / Plasma / Electromagnetic wave / CFD / CEM / Reaction
Research Abstract

We estimated microwave attenuations by a solid rocket motor plumes, assuming that the attenuation is caused by (I)Aluminum/Alumina particles, and (2)free electrons. The expressions and values of the attenuations show that the microwave attenuation observed in real rocket motors is caused by free electorons.
We analyzed the plume of the H-IIA SRB-A solid rocket motor plume numerically. The numerical model includes a chemical reaction model of the plume gas. The numerical result shows that the chemical reactions are frozen and the mole fraction of electron is constant through the nozzle ; the electron number density is calculated from the pressure and temperature of the gas. The electron mole fraction is strongly depends on the amount of impurity, such as the sodium, in the motor grain
We analyzed microwave propagation in the weakly-ionized plume gas using a two dimensional GEM (Computational Electro Magnetics) model. Results show that (1)the effect of diffraction and refraction of microwave cannot be neglected, (2)the microwave attenuation depends weakly on the microwave frequency, (3)the microwave attenuation is proportional to electron number density, and (4)the microwave attenuation is in inverse proportion to the electron collision frequency.
We conducted a microwave attenuation measurement in the ground firing tests. The theoretical results agrees quantitatively with the experimental result. The electron mole fraction estimated from the experimental result is I order less than that of the theoretical result ; the cause of it is considered the impurities were less than the assumed amount. No modulation of microwave is observed in the received microwave which propagates through the motor plume.

  • Research Products

    (8 results)

All Other

All Publications (8 results)

  • [Publications] T.Abe, K.Fujita, H.Ogawa, I.Funaki: "Microwave telemetry breakdown caused by rocket plume"AIAA Paper. 2000-2484. 1-6 (2000)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] I.Funaki, H.Ogawa, T.Kato, T.Abe, K.Fujita, S.Nonaka: "Microwabe attenuation measurement of full scale solid rocket motor plumes"AIAA paper. 2002-2241. 1-10 (2002)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] H.Ogawa, I.Funaki, T.Kato, T.Abe, K.Fujita, S.Nonaka: "Microwabe attenuation measurement of full scale solid rocket motor plumes"Proceedings of 23^<rd> ISTS. 2002-e-48. 1-7 (2002)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] 小川博之, 徳留真一郎, 寺本進, 藤田和央: "M-14モータノズルへの熱入力の評価"宇宙科学研究所SESデータセンター,SES-TN-00-001. 90 (2000)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] T.Abe, K.Fujita, H.Ogawa, I.Funaki: "Microwave telemetry breakdown caused by rocket plume"AIAA paper. 2000-2484. 1-6 (2000)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] I.Funaki, H.Ogawa, T.Kato, T.Abe, K.Fujita, S.Nonaka: "Microwave attenuation measurement of full scale solid rocket motor plumes"AIAA paper. 2002-2241. 1-10 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] H.Ogawa, I.Funaki, T.Kato, T.Abe, K.Fujita, S.Nonaka: "Microwave attenuation measurement of full-scale solid rocket motor plumes"Proceedings of 23^<rd> ISTS. 2002-e-48. 1-7 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] H.Ogawa, S.Tokutome, S.Teramoto, K.Fujita: "Estimation of heat flux on M-14 solid rocket motor nozzle wall (in Japanese)"ISAS SES DATA CENTER. SES-TN-00-001. 1-90 (2000)

    • Description
      「研究成果報告書概要(欧文)」より

URL: 

Published: 2005-04-19  

Information User Guide FAQ News Terms of Use Attribution of KAKENHI

Powered by NII kakenhi